|Publication number||US7717593 B2|
|Application number||US 11/760,386|
|Publication date||May 18, 2010|
|Filing date||Jun 8, 2007|
|Priority date||Jun 8, 2007|
|Also published as||US20080304273|
|Publication number||11760386, 760386, US 7717593 B2, US 7717593B2, US-B2-7717593, US7717593 B2, US7717593B2|
|Original Assignee||The Boeing Company|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (36), Non-Patent Citations (3), Referenced by (5), Classifications (19), Legal Events (2)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The disclosure relates to interior illumination systems for aircraft, particularly interior illumination and lighting systems for the passenger cabins in commercial passenger airplanes.
The interior configuration, architecture, and illumination of airplanes has become relatively standardized today. The arrangement of passenger seats, passenger cabins, bulkheads, lavatories, serving areas, and the like have become developed for convenience and accommodation of both passengers and crew. Passenger compartments typically have sidewall members with a plurality of windows, a floor member and a ceiling member or assembly of some type. In addition, pluralities of rows of stowage or storage bins are positioned on the aircraft generally at the position between the sidewalls and the ceilings. For larger twin-aisle aircraft, rows of inboard stowage bins are also positioned over the seats located along the center of the passenger cabins.
The design, architecture, and lighting of the interiors of passenger aircraft, particularly the passenger cabins, have remained substantially the same for a long period of time and have not had a significant variety of changes or updates.
There continues to be a need in the aircraft industry for new and innovative solutions to passenger space, cabins, furnishings and illumination. There is also a need to change or vary the aesthetics of passenger cabins in order to improve the perception and aesthetics of the space, as well as possibly catering to the different moods of the passengers. This includes the use of changes in LED based mood lighting to emphasize the activities performed aboard an aircraft, such as boarding, resting, eating and the like.
The improvements described herein would be particularly useful in an aircraft cabin illumination system such as described in co-pending patent application Ser. No. 11/553,725 filed Oct. 27, 2006, which is a continuation of Ser. No. 11/164,267 filed Nov. 16, 2006, now abandoned. Both of these applications are incorporated herein by reference.
A large number of illumination systems employ a wide variety of light emitting diode (LED) illumination subsystems. These include those with relatively simple beam forming optical surfaces, such as seen for example U.S. Pat. Nos. 7,083,297, 7,059,731, 6,899,443, 6,988,815, 6,896,381, 6,819,506 and 6,814,470. Other beam forming optics, with more unusual shapes, including faceted surfaces are disclosed in U.S. Pat. Nos. 7,042,655, 7,021,767, 7,006,306, 6,924,943, and 6,607,286. Also, simple strip light illumination systems are disclosed, for example in U.S. Pat. Nos. 7,114,827, 7,063,440 and 6,609,813. All of the aforementioned U.S. patents are incorporated herein by reference.
However, none of these prior designs include offset beam apertures that improve the coupling efficiency of beam forming optics as practiced in embodiments of this disclosure.
Aircraft can be designed with an all LED interior lighting system and this allows the aircraft manufacturer to take advantage of the unique properties of LED lighting and to make significant advances in cabin illumination capabilities compared to conventional illumination systems based on fluorescent and incandescent sources. Specifically embodiments of this disclosure use improved LED-based lighting systems to enhance the configuration, architecture, illumination and aesthetics of passenger space of the aircraft. The improved LED-based system may be an LED modified with efficient beam-forming optics. An important feature that has been developed to achieve these improvements is the development of cross bin lighting in which the overhead storage bins are illuminated with one color and the ceiling structure between the bins is illuminated with another color. These colors may be varied during flight, but a typical passenger-pleasing color configuration may be white light illumination for the overhead bins and blue light for the ceiling area. Another important feature of the present design is that the light sources should not generally be visible to passengers in the cabin.
Additionally, any illumination system used on an aircraft is preferably both lightweight and efficient in the use of electrical power. Illumination systems based on light emitting diodes (LEDs) offer considerable advantages over conventional fluorescent or incandescent illumination sources in this regard. These include smaller source size, lower electrical power consumption and longer operating lifetimes. However, LEDs generally emit light in a different angular pattern compared to conventional sources. The efficient use of LED illumination systems therefore requires optimization of the coupling of the LED source light output into a useful illumination beam. Embodiments of this disclosure also provide novel and efficient optical means for coupling LED light sources into useful illumination beams.
Furthermore, the need to hide a cross bin lighting system from general passenger view imposes constraints on the size and placement of the light sources used for this application. The basic requirement is that the lighting sources must be placed behind a valence or similar line of sight obstruction situated on top of the overhead bins and below a plane that extends from the top of one valence to a tangent point along the lower curve of the opposite overhead bin.
The embodiments of the disclosure provide efficient beam forming optics that work in situations that have line of sight source height restrictions, such as those found in aircraft cabin cross bin lighting. In such situations, the beam coupling efficiency may be improved by using larger beam forming optics and restricting the working source height with an aperture that selects only part of the full height. Generally these apertures are not placed along the center line of the beam forming optic.
Thus, embodiments of this disclosure utilize an improved LED illumination system with efficient beam-forming optics to provide a coupling design which facilitates cross cabin illumination while remaining out of view from the passengers' perspective.
Cross-bin illumination may be provided by a set of lights on each side of the ceiling structures which direct their illumination across the ceiling space to the opposite sets of storage/stowage bins. The illumination from these lights may be directed across and under the ceiling to illuminate the storage/stowage bins (or monument or surface) located opposite from the light fixture. Typically, the color of the illumination from these lights is white but this may be changed to other colors to set specific lighting moods. A second set of lights is used to illuminate the ceiling. Typically, color of these lights is blue, but this may also be changed to set specific lighting moods. Together, the illumination from the two sets and two pairs of lights provides ceiling and cross bin illumination as necessary.
The two or more sets or arrays of the improved LEDs with efficient beam-forming optics can be positioned in various configurations, such as but not limited to being stacked one on top of the other, positioned individually side-by-side, or positioned in groups side by side. In practice an array of such LEDs with efficient beam-forming optics can run the length of an aircraft cabin.
Further details, benefits and features of embodiments of this disclosure will become apparent from the following description when taken in connection with the accompanying drawings and appended claims.
The need to hide aircraft cross bin lighting from general passenger view imposes restrictions on the size and placement of the light sources used for this application. The basic requirement is that the lighting sources may be placed behind a valence situated on top of the overhead bins and below a plane that extends from the top of one valence to a tangent point along the lower curve of the opposite overhead bin.
Disclosed in detail below is an LED-based illumination system having efficient beam-forming optics for improved lighting in areas where there are line-of-sight source height restrictions, such as those found in aircraft cabin cross bin lighting. The subject design provides a significant increase in optical coupling efficiency by making the area of the beam forming optics larger than the area allowed by valence line of sight restrictions. An aperture is used to select only a portion of the available area. The selection of the specific aperture area is determined by the optical properties of the LED source.
It is known in the art of illumination system design that there is a basic relationship between the area of an illumination optic and its associated beam divergence angle. This may expressed mathematically in the form:
A1 Sin2 θ1=A2 Sin2 θ2
where A is area of the cross section of the beam shaping optic and θ is the divergence angle. The quantity A Sin2 θ is known variously as the etendue or Lagrange invariant. The expression means that an illumination beam with a small area cross section and a large divergence angle can only be converted into a beam with a smaller divergence angle by increasing the cross section area of the beam forming optic. This is a fundamental relationship that does not depend upon the detailed shape of the optical surfaces involved.
The subject efficient beam forming optical LED 1 may include any suitable beam shaping element 4 in which the surfaces are curved, flat or faceted. Surface 11 may also be made reflective by other means such as coating so that its shape is not limited by the need for total internal reflection. The aperture formed between members 3 and 3A may be any suitable shape that meets the light source height limitation and optimizes the beam coupling efficiency. Beam forming optics for LED devices are available from a variety of commercial sources including Carclo Precision Optics which is part of the Technical Plastics Division of Carclo plc of Berkshire, England, and Polymer Optics Limited, also of Berkshire, England. Injection molded polycarbonate optics will be particularly useful in the subject aircraft illumination applications.
Beam paths 20 and 21 clearly show that light emitted by the LED at large angles from the optical axis exits the beam forming optic 4 at a different spatial location compared to that emitted from the LED at narrow angles. Beams 20A and 21A illustrate the LED output and beam divergence for beams 20 and 21 respectively.
The need to place the cross bin light source below a valence plane and yet still make the area of the source large enough to provide a necessary narrow beam size for illumination presents conflicting design requirements that compromise the optical coupling efficiency of the system. Embodiments of this disclosure achieve a significant increase in optical coupling efficiency gained when the area of the beam-forming optics is made larger than the area allowed by a valence line-of-sight restriction. An aperture is used to select only a desired portion of the available area. The selection of a specific aperture area must be varied in accordance with the optical properties of the selected LED source.
The beam-forming optics of the new illumination system will be better understood in the context of deployment in a passenger aircraft cabin. The passenger compartments of commercial airlines today have become relatively standardized. The space in passenger cabins is quite limited due to the external fuselage size and the configuration of the airplane itself.
An aircraft passenger cabin will typically have a floor panel, a pair of sidewall members or panels, a ceiling panel or structure, and a plurality of passenger seats. As is common with larger commercial passenger airliners today, the passenger seats in each row are often arranged in three sets, with two aisles.
The exterior of the typical airplane fuselage is clad with an exterior skin which is attached to longeron and/or frames and/or bulkhead members or other structure. The bulkhead members provide support and stability for the fuselage of the aircraft.
The passenger cabin has a plurality of rows of outboard storage or stowage bins, which are provided generally at the intersection of the sidewall members and the ceiling structure. If the airplane has a twin-aisle passenger cabin, rows of inboard storage bins are also provided over the central row of passenger seats. The storage/stowage bins door or bins themselves may be hinged relative to the passenger cabin such that they rotate from an up or closed position to a down or open position. The storage/stowage bins are used for storing luggage, packages, and other personal items of the passengers during flight.
The ceiling system of a two-aisle aircraft has a central structure in which the two inboard storage/stowage bins are positioned above the central section of passenger seats. The central ceiling structure may be suspended and held in place in the aircraft by conventional strut members. In one embodiment, additional ceiling structures are positioned between the central stowage bins and the two rows of outboard storage/stowage bins.
Inboard stowage bin 42A is also depicted in its lowered position 42B by the interrupted lines. In this regard, the structure and configuration of the ceiling panel 52A, together with the wall panel members 76 and 78 position the lighting elements 72A, 72B, 74A and 74B at positions such that they cannot typically be viewed by the passengers in the passenger cabin. In this embodiment, structural surface 76 may be considered a valance structure for obstructing a passenger from directly viewing light emitted from lighting fixtures 72A and 74A.
In this embodiment, the lighting fixtures 72A, 74B may be the subject efficient beam-forming optical LEDs, preferably utilizing RGBW-type lighting in this application and which are directed to focus their illumination on the ceiling panel 52A. For example, in the case of fixture 74B, its beam is indicated by the arrows 80 in
The surface of the ceiling member 52A can be illuminated in any color without limitation, such as blue emulating the sky, while the rest of the area below is illuminated in white light or another light color.
The pairs of lighting fixtures 72A and 74A on the one hand and 72B and 74B on the other can provide uniform illumination of the ceiling without areas of significantly different intensities. The pairs of lighting fixtures may also allow illumination in the passenger cabin below the ceiling panels in a more uniform and pleasant manner. The cross bin lighting system utilizing the LEDs with efficient beam-forming optics, as shown in
In the embodiment of the disclosure depicted in
Embodiments allow better directional control of the light beams within the passenger cabin, and the alternate use of colored light produces effects within the cabin which are pleasing to the passengers and also create the impression of space and height.
An LED device commonly used for illumination applications is a Luxeon batwing-type LED, Model LXHL-BW02, which is a white emitter device commercially available from Phillips Lumileds Lighting Company, San Jose, Calif. The expression “batwing” refers to the typical pattern of a graph of its spatial radiation when relative intensity is plotted against angular displacement in degrees from its optical center. According to data published by the manufacturer, the LED Model LXHL-BW02 has intensity peaks near 40° angular displacement on either side of its optical axis.
When this LED is used in combination with beam forming optic 4 described in connection with
As discussed above,
In an application of the lighting system of this type, the data described in
In a particular cross bin illumination application utilizing the beam forming optic, the allowable height behind the valence is only 9 mm. In
Light source assembly 501 also has a second source fixture 506 which utilizes the efficient beam-forming optical LED illumination device described in connection with the earlier figures. The efficient beam forming optical LED is configured to avoid any line of sight (L.O.S.) restrictions 508 and thereby effectively illuminate opposite stowage bin 511. A fourth light source fixture 507, also utilizing an efficient beam forming optical LED operates similarly to provide the intended cross bin illumination, while avoiding visible glare and the other problems discussed above.
While the illumination device and system has been described in connection with one or more embodiments, it is to be understood that the specific mechanisms and techniques which have been described are merely illustrative and numerous modifications may be made to the methods and apparatus described without departing from the spirit and scope of the improvements defined by the appended claims.
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|U.S. Classification||362/471, 362/484, 362/470, 362/490|
|International Classification||F21V21/00, B60Q1/00, B64F1/20, B64D47/02, B60Q3/00|
|Cooperative Classification||B64D11/00, F21V5/04, F21V7/0091, B64D2011/0038, B60Q3/025, F21Y2101/02|
|European Classification||B60Q3/02D2, F21V7/00T, F21V5/04, B64D11/00|
|Jun 8, 2007||AS||Assignment|
Owner name: BOEING COMPANY,ILLINOIS
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:CLARK, ROY;REEL/FRAME:019403/0357
Effective date: 20070607
|Nov 18, 2013||FPAY||Fee payment|
Year of fee payment: 4